| Patents for B64C 21 - Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (1,724) |
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| 05/05/2010 | EP1976743B1 Device for reducing a drag produced by the relative displacement of a body and fluid |
| 05/04/2010 | US7708230 Flow distribution system for inlet flow control |
| 04/29/2010 | WO2010046679A1 Bluff body noise control |
| 04/28/2010 | EP2179903A2 Method of creating the power system for a multi-purpose means of transport and multi-purpose means of transport to implement the method |
| 04/28/2010 | EP2178747A2 Translating flap drive door |
| 04/21/2010 | EP2176125A1 Reducing the boundary layer of aerodynamic effects |
| 04/21/2010 | EP2176124A2 Electromagnetic transduction acoustic bridge |
| 04/08/2010 | US20100084514 System and method to control flowfield vortices with micro-jet arrays |
| 04/01/2010 | WO2009143518A3 Boundary layer control system and methods thereof |
| 04/01/2010 | US20100078522 Apparatus, system and method for drag reduction |
| 03/31/2010 | EP2168869A1 Device for reducing the cross-stream force generated by the section of air refuelling booms |
| 03/30/2010 | US7686257 Dual bimorph synthetic pulsator |
| 03/30/2010 | CA2435173C Method and apparatus for modulating flow separation |
| 03/18/2010 | WO2010029844A1 Structure for reducing fluid resistance by roughening object surface |
| 03/10/2010 | EP2160324A1 A method for increasing the lift of aerodynamic surfaces and for reducing the drag |
| 03/09/2010 | US7673834 Vortex ring generator |
| 03/09/2010 | US7673832 Aircraft component exposed to streaming surrounding air |
| 03/04/2010 | WO2010024726A1 Method for producing thrust (embodiments) and apparatus for travel in a fluid medium (embodiments) |
| 03/04/2010 | WO2010005341A3 Hollow wing with an air intake in the leading edge |
| 03/04/2010 | US20100051754 Aircraft |
| 03/04/2010 | DE102008039061A1 Device for separation of turbulent limit layer of fuselage from front edge of wing of e.g. aircraft, has separation edge perpendicular to flow, where device is bordered by fuselage surface and surface perpendicular to support surface |
| 02/25/2010 | US20100044520 Establishment of laminar boundary layer flow on an aerofoil body |
| 02/17/2010 | EP2153065A2 Turbine blade protective barrier |
| 02/16/2010 | US7661629 Systems and methods for destabilizing an airfoil vortex |
| 02/11/2010 | DE102008037142A1 Ausfahrbarer Abweiser zum Freisetzen von Struktur schädigenden Fluiden Extendable deflector for releasing structure harmful fluids |
| 02/04/2010 | WO2008098332A3 Vortex generator for flush air inlets performance improvement |
| 02/03/2010 | CN100586793C Aerodynamic body |
| 01/21/2010 | WO2009088780A3 Systems and methods for controlling flows with pulsed discharges |
| 01/14/2010 | WO2010005341A2 Use of positive pressure inside a flexible wing for blowing off some of the incoming flow through a shaped slit to the upper surface thereof |
| 01/14/2010 | US20100006707 Advanced Trailing Edge Control Surface on the Wing of an Aircraft |
| 01/13/2010 | CN201380960Y Single hole micro-blowing perturbation active control device for asymmetric vortices at high angle of attack |
| 01/07/2010 | US20100004799 Systems and Methods for Alleviating Aircraft Loads with Plasma Actuators |
| 01/06/2010 | CN100577513C System for aerodynamic flows and associated method |
| 01/05/2010 | US7641144 Cross-flow fan propulsion system |
| 12/31/2009 | US20090321580 Vernier active flow control effector |
| 12/30/2009 | EP2137068A2 Laminar flow surfaces with selected roughness distributions, and associated methods |
| 12/29/2009 | US7637462 Surface flow diverting and static charging ducted pores on wing or blade tip to reduce wake and BVI noise |
| 12/22/2009 | US7635107 System for aerodynamic flows and associated method |
| 12/17/2009 | WO2009124728A3 Flow element, and high-lift system comprising such a flow element |
| 12/17/2009 | US20090308980 Method and system for fully fixed vehicle control surfaces |
| 12/03/2009 | US20090294596 Method of Reducing Drag and Increasing Lift Due to Flow of a Fluid Over Solid Objects |
| 12/02/2009 | EP2125511A1 Surface structure |
| 11/26/2009 | WO2009143518A2 Boundary layer control system and methods thereof |
| 11/26/2009 | US20090289150 Boundary layer control system and methods thereof |
| 11/25/2009 | EP2121436A2 Vortex generator for flush air inlets performance improvement |
| 11/19/2009 | WO2009138773A1 Airfoil with flow deflector |
| 11/19/2009 | CA2721276A1 Airfoil with flow deflector |
| 11/12/2009 | WO2009137143A1 Passive adaptive structures |
| 11/12/2009 | WO2009080355A4 Lift system for an aircraft comprising a main wing and an adjustable slat |
| 11/10/2009 | US7614588 Apparatus system and method for drag reduction |
| 10/29/2009 | US20090266937 Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows |
| 10/22/2009 | US20090261206 Method of using microjet actuators for the control of flow separation and distortion |
| 10/15/2009 | WO2009124728A2 Flow element, and high-lift system comprising such a flow element |
| 10/15/2009 | DE102008017574A1 Strömungskörper und Hochauftriebssystem mit einem solchen Strömungskörper Flow body and high-lift system with such a flow body |
| 10/15/2009 | CA2720657A1 Aerodynamic body and high-lift system comprising such an aerodynamic body |
| 10/08/2009 | WO2009121986A1 Aerodynamic thrust element |
| 10/01/2009 | DE102008016399A1 Flying object i.e. aircraft, has surfaces at which air turbulences are formed, where elastic coating is formed over surfaces and elastic filling is provided between fixed surface and elastic skin |
| 09/29/2009 | US7594625 Proprotor blade with leading edge slot |
| 09/24/2009 | WO2009080355A3 Lift system for an aircraft comprising a main wing and an adjustable slat |
| 09/16/2009 | CN101531251A An aircraft safeguard protection device |
| 08/27/2009 | US20090212165 Passive removal of suction air for laminar flow control, and associated systems and methods |
| 08/27/2009 | US20090212164 Airfoil trailing edge plasma flow control apparatus and method |
| 08/26/2009 | EP2091814A1 Establishment of laminar boundary layer flow on an aerofoil body |
| 08/20/2009 | WO2009101001A1 Method for actively deforming an aerodynamic profile |
| 08/20/2009 | WO2009100643A1 Movement apparatus |
| 08/20/2009 | US20090210103 Controlling aircraft aerial movements, defeating icing on aircraft surfaces, aiding decontamination, and damping turbulence effects on aircraft by the method of micro-perforated airfoil coordinated precision flow management |
| 08/20/2009 | US20090206206 Highly efficient supersonic laminar flow wing |
| 08/20/2009 | CA2715116A1 Method for actively deforming an aerodynamic profile |
| 08/19/2009 | CN101511673A Panel assembly and method of erecting a panel assembly |
| 08/18/2009 | CA2446714C Aerofoil with gas discharge |
| 08/13/2009 | DE102008006437A1 Aerodynamisches Hochleistungsprofil für Luftfahrzeuge The aerodynamic high-performance profile for aircraft |
| 08/12/2009 | EP2086831A2 Device for delaying boundary layer separation |
| 08/05/2009 | EP1966044B1 Controlling the boundary layer of an airfoil |
| 07/30/2009 | US20090189023 Aerodynamic high-performance profile for aircraft |
| 07/16/2009 | WO2009088780A2 Systems and methods for controlling flows with pulsed discharges |
| 07/09/2009 | WO2009085418A1 Methods for reducing laminar flow disturbances on aerodynamic surfaces and articles having self-cleaning aerodynamic surfaces |
| 07/09/2009 | WO2009083622A1 System and method for reducing the frictional resistance of fluids on the surface of boats and aircraft |
| 07/09/2009 | US20090173837 Systems and methods for controlling flows with pulsed discharges |
| 07/09/2009 | CA2709917A1 Methods for reducing laminar flow disturbances on aerodynamic surfaces and articles having self-cleaning aerodynamic surfaces |
| 07/08/2009 | EP2076434A1 Object with surface for generating micro swirls |
| 07/02/2009 | WO2009080168A1 Aircraft cooling system |
| 07/02/2009 | CA2709766A1 Aircraft cooling system |
| 06/25/2009 | WO2009079046A2 Systems and methods for control of engine exhaust flow |
| 06/25/2009 | WO2009077690A2 Aircraft nacelle including an optimised ice treatment system |
| 06/25/2009 | WO2009077689A2 Air outlet system for aircraft leading edge |
| 06/25/2009 | WO2009077688A2 Aircraft nacelle including hot air discharge means |
| 06/25/2009 | US20090159754 Rotary wing system with ion field flow control |
| 06/25/2009 | CA2707655A1 Aircraft nacelle including an optimised ice treatment system |
| 06/25/2009 | CA2707636A1 Air outlet system for aircraft leading edge |
| 06/25/2009 | CA2707501A1 Aircraft nacelle including hot air discharge means |
| 06/23/2009 | CA2434949C Method and apparatus for modulating airfoil lift |
| 06/17/2009 | EP1868890B1 Reduction of frictional losses in the region of boundary layers on surfaces, around which a fluid flows |
| 06/11/2009 | WO2008134151A3 Laminar flow surfaces with selected roughness distributions, and associated methods |
| 06/10/2009 | EP2066564A1 Vertical take-off and landing vehicle which does not have a rotary wing |
| 06/10/2009 | CN101454202A Aerodynamic flap of an aircraft with a device which influences the flap turbulence |
| 05/28/2009 | WO2009023354A3 Passive removal of suction air for laminar flow control, and associated systems and methods |
| 05/28/2009 | DE102007054873A1 Umlenkvorrichtung zur Vermeidung der Kontamination der Grenzschicht auf Tragflächen eines Flugkörpers in Unter- und Transschallströmung durch den Rumpf oder ähnliche Körper Deflection to avoid contamination of the boundary layer on the wings of a flying object in the lower and transonic flow through the torso or similar body |
| 05/27/2009 | CN101443233A Reinforced hybrid structures and methods thereof |
| 05/26/2009 | US7537182 Simultaneous multiple-location separation control |
| 05/21/2009 | US20090127403 Lift flap carrier system |